ES2355167T3 - Turbina para una turbina de gas. - Google Patents

Turbina para una turbina de gas. Download PDF

Info

Publication number
ES2355167T3
ES2355167T3 ES07801309T ES07801309T ES2355167T3 ES 2355167 T3 ES2355167 T3 ES 2355167T3 ES 07801309 T ES07801309 T ES 07801309T ES 07801309 T ES07801309 T ES 07801309T ES 2355167 T3 ES2355167 T3 ES 2355167T3
Authority
ES
Spain
Prior art keywords
turbine
holes
blade
guide vanes
crown
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
ES07801309T
Other languages
English (en)
Spanish (es)
Inventor
Fritz Kennepohl
Detlef Korte
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MTU Aero Engines AG
Original Assignee
MTU Aero Engines GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by MTU Aero Engines GmbH filed Critical MTU Aero Engines GmbH
Application granted granted Critical
Publication of ES2355167T3 publication Critical patent/ES2355167T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/16—Form or construction for counteracting blade vibration
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Separation By Low-Temperature Treatments (AREA)
ES07801309T 2006-09-12 2007-09-01 Turbina para una turbina de gas. Active ES2355167T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102006042647A DE102006042647A1 (de) 2006-09-12 2006-09-12 Turbine einer Gasturbine
DE102006042647 2006-09-12

Publications (1)

Publication Number Publication Date
ES2355167T3 true ES2355167T3 (es) 2011-03-23

Family

ID=38988314

Family Applications (1)

Application Number Title Priority Date Filing Date
ES07801309T Active ES2355167T3 (es) 2006-09-12 2007-09-01 Turbina para una turbina de gas.

Country Status (6)

Country Link
US (1) US9103216B2 (de)
EP (1) EP2061953B1 (de)
AT (1) ATE495346T1 (de)
DE (2) DE102006042647A1 (de)
ES (1) ES2355167T3 (de)
WO (1) WO2008031395A1 (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201707836D0 (en) * 2017-05-16 2017-06-28 Oscar Propulsion Ltd Outlet guide vanes
EP3799030B1 (de) * 2019-09-26 2024-11-27 Rolls-Royce Deutschland Ltd & Co KG Akustische auskleidung und gasturbinenmotor mit solch einer akustischen auskleidung
US11408349B2 (en) 2020-08-14 2022-08-09 Raytheon Technologies Corporation Active flow control transpirational flow acoustically lined guide vane
US11512608B2 (en) * 2020-08-14 2022-11-29 Raytheon Technologies Corporation Passive transpirational flow acoustically lined guide vane

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1829674A (en) * 1928-12-08 1931-10-27 Gen Electric Elastic fluid turbine and the like
US3527543A (en) * 1965-08-26 1970-09-08 Gen Electric Cooling of structural members particularly for gas turbine engines
GB1225771A (de) 1967-03-28 1971-03-24
CH584347A5 (de) * 1974-11-08 1977-01-31 Bbc Sulzer Turbomaschinen
GB2026622A (en) * 1978-07-08 1980-02-06 Rolls Royce Blade for Fluid Flow Machine
US4303374A (en) * 1978-12-15 1981-12-01 General Electric Company Film cooled airfoil body
JPH0660562B2 (ja) 1983-05-26 1994-08-10 株式会社東芝 ガスタ−ビン空冷翼
DE3505823A1 (de) 1985-02-20 1986-08-21 Hans 8038 Gröbenzell Bischoff Anordnung zur beeinflussung der stroemung an leit- oder laufschaufeln fuer turbomaschinen
US4672727A (en) * 1985-12-23 1987-06-16 United Technologies Corporation Method of fabricating film cooling slot in a hollow airfoil
US4669957A (en) * 1985-12-23 1987-06-02 United Technologies Corporation Film coolant passage with swirl diffuser
JP2615823B2 (ja) * 1988-04-28 1997-06-04 松下電器産業株式会社 羽根車の翼型ブレードの製造方法
US5480284A (en) * 1993-12-20 1996-01-02 General Electric Company Self bleeding rotor blade
US6004095A (en) * 1996-06-10 1999-12-21 Massachusetts Institute Of Technology Reduction of turbomachinery noise
DE19821770C1 (de) * 1998-05-14 1999-04-15 Siemens Ag Verfahren und Vorrichtung zur Herstellung eines metallischen Hohlkörpers
US6139259A (en) 1998-10-29 2000-10-31 General Electric Company Low noise permeable airfoil
US6422819B1 (en) * 1999-12-09 2002-07-23 General Electric Company Cooled airfoil for gas turbine engine and method of making the same
GB2361035A (en) * 2000-04-07 2001-10-10 Rolls Royce Plc Gas turbine engine vane with noise attenuation features
US7018172B2 (en) 2003-12-22 2006-03-28 United Technologies Corporation Airfoil surface impedance modification for noise reduction in turbofan engines
US7320575B2 (en) * 2004-09-28 2008-01-22 General Electric Company Methods and apparatus for aerodynamically self-enhancing rotor blades

Also Published As

Publication number Publication date
US9103216B2 (en) 2015-08-11
DE502007006261D1 (de) 2011-02-24
EP2061953A1 (de) 2009-05-27
DE102006042647A1 (de) 2008-03-27
ATE495346T1 (de) 2011-01-15
US20100202890A1 (en) 2010-08-12
WO2008031395A1 (de) 2008-03-20
EP2061953B1 (de) 2011-01-12

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